NORTH AMERICAN American T28C Piston SOLD

Airframe: 9765 Hrs TTSNEW Engine(s): Curtiss-Wright R-1820-86B 765 Hrs SMOH by Precision Engines Complete Firewall Forward in conjunction with Engine rebuild Avionics: Garmin SL-40 COMM Garmin GA-35 WAAS Garmin GTN-750XI Touch GPS/NAV/COMM Garmin GNC-355A GPS/COMM (REAR) Garmin GNC-355A GPS/COMM (FRONT) GI-275 HSI (FRONT AND REAR) (2) Garmin GI-275 (FRONT) (2) Garmin GI-275 (REAR) Garmin GFC-500 Autopilot KR-22 Marker Beacon King KN-69 DME Stormscope Garmin GTX-345D ADS-B Out Transponder ELT 345 Equipment: Large Nose Wheel Assembly Pre-Oiler Cleveland Brakes Custom Seat Cushions Oil Scavenge System Dual Rotating Beacons Smoke System-10 Gallon Tank Oil Shut-off System with starter interlock Whelen Strobes New Poly Carbonite Windscreens Hooker 5 point Harness system Reiff Oil Tank and Cylinder Heater System New Oxygen System MX tracking logbooks in planelogix.com All T-28 Maintenance Manuals from NATA included Propeller(s): Hamilton Standard 43D50 with Super B Blades 765 Hours SPOH, AD 81-13-06R2 next due 3/2024 Miscellaneous: Annual Inspection Completed May 2022 VFR Transponder inspection completed July 2022 IFR Certified Exterior: Jet-Glo Navy Gray with White undersides in good condition, NATC (Naval Air Training Command) colors Interior: Total Restoration, Finished in Light Grey Epoxy in Excellent Condition DETAILS OF RESTORATION: General: Aircraft Completely Disassembled Aircraft Paint Stripped Inside and Out All Wiring, Hardware, Brackets etc. Removed Aircraft Inspected for Corrosion Wings Rework and Overhaul: Overhauled Fuel Cells and Tank Hardware Installed All Flexible Fuel lines & Fittings Replaced with New Aircraft completely Re-wired using all New Wire and Cannon plugs Inboard Wing Attach Points and Joining Lugs Inspected for Cracks using DPI inspection method Top Trailing Edge Skins and Trailing Edge Extrusion Replaced between Sta.28.2 to Sta.153.9 Leading Edge Skins Replaced Sta.28.8 to Sta.153.9 left and right hand Wing Sections Joined together with New NDI, Inspected Bolts I.A.W. T.O. IT-28B-2 Fuel Quantity Senders and Computer Calibrated and Installed Main Landing Gear and Hydraulic Components Overhauled and Installed Fuselage: Fuselage Primed Inside and Out Fuselage Re-wired using all new Wiring and Cannon Plugs All New Control Cables, Pulleys and Hardware Installed Engine Control Push Rods Rebuilt and Installed using all New Hardware and Rod End Bearings Tail Cone Mated to Fuselage Using New Attach Hardware Vertical Stabilizer Installed All Hydraulic Components Overhauled, Bench Tested and Installed All Airframe Fluid Carrying Hoses Installed Nose Gear and Components Overhauled, Painted and Installed Wings Mated to Fuselage Using New Hardware per T.O. IT-28B-2 Bearings Replaced as Necessary Flaps Reskinned and New Trailing Edge Extrusion Installed Ailerons Painted and Balanced and Installed with New Hardware Rudder Painted and Balanced and Installed with New Hardware All Flight and Engine Controls Rigged per T.O. IT-28B-2 New Static Dischargers Installed